N813FD

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 45,229 hrs · 19,989 cycles

LT WING INBD FLAP LWR SKIN JUST AFT OF THE CARRIAGE FOUND PUNCTURED. CUT OUT THE DAMAGED LOWER SKIN PER SRM 57-52-12/201 FIG205.

Part: SKIN — CHAFED (RT WING) · airframe 45,229 hrs · 19,989 cycles

FLUSH DOUBLER REPAIR ON L/E OF D-NOSE SKIN CHAFED AT TRACK NR 1. REPAIRED IAW EA6-5741-103419

Part: FITTING — CORRODED (NR 1 NACELLE) · airframe 45,229 hrs · 19,989 cycles

NR 1 ENG PYLON SPIGOT RECEPTACLE UPPER AND LOWER FITTING CORRODED. REMOVED THE SPIGOT FITTINGS PER SRM51-40-21 MACHINE THE MATING SURFACE OF THE NEW SPIGOT LOWER FITTING PER DWG A54611053. HORNED THE BORES C/T THE LOWER AND UPPER SPIGOT FITTINGS PER DWG A54611821. PERFORMED FLUORESCENT DYE MAGNETIC PARTICLE INSPECTION OF THE MACHINED SURFACE PER NTM51-80-00, NO CRACKS FOUND. PICKED UP HOLES C/T THE LOWER AND UPPER SPIGOT FITTINGS, BROKE SHARE EDGES AND DEBURRED HOLES PER SRM 51-40-44. CADMIUM PLATED THE REWORKED AREA PER SRM 51-21-10. APPLED PRIMER AND TOPCOAT ON THE REWORKED SURFACE PER SRM 51-23-00. APPLED SEALANT TO THE MATING SURFACES OF FITTINGS PER SRM 51-24-00. INSTALLED THE SPIGOT LOWER AND UPPER FITTINGS AS PER DWG A54611821 & SRM51-40-21.

Part: ANGLE — CRACKED (CENTER WING) · airframe 45,229 hrs · 19,989 cycles

CENTER WING FUEL TANK REAR SPAR INNER ANGLE FOUND CRACKED. REPAIRED IAW SRM 51-40-44, EO 6-5710-7-3322 &SRM 51-40-21. NO CRACK FOUND IAW NTM51-10-18.

Part: ANGLE — CRACKED (CENTER WING) · airframe 45,229 hrs · 19,989 cycles

CENTER WING FUEL TANK REAR SPAR INTERNAL ANGLE FOUND CRACKED. COMPLIED WITH EA 6-5710-153425. REAMED HOLE IAW EA:6-5710-7-3322, B1, PART 1.

Part: SLAT TRACK — DAMAGED (LT NR 3 SLAT) · airframe 45,229 hrs · 19,989 cycles

LEFT WING SLAT NR 3, NR 9 TRACK BLEND OUT AREA EXCEEDED THE LIMITS (WIDTH=56.21MM). COMPLIED WITH EA 6-5741-103381, PART 3. REPLACED SLAT TRACK IAW AMM27-80-14-04. PERFORMED TEST OF SLAT IAW AMM27-80-14-04. TESTED OK.

Part: FLUID — ODOR (DE ICE SYSTEM) · airframe 44,727 hrs · 19,641 cycles

ON TAKEOFF AT 4000FT. ECAM ALERT OF MAIN DECK CARGO SMOKE. FOLLOWED QRH AND RETURNED TO DEPARTURE. WE HAD EXTENSIVE ICE ON ACFT WHICH REQUIRED 1 HR 45 MIN OF DEICING. EMERGENCY DECLARED. IAW CREW DEBRIEF, SMOKE INDICATIONS CEASED. VERY STRONG ODOR OF DEICE FLUID IN ACFT. NO HOT INDICATIONS WERE FOUND DURING FIRE DEPARTMENT INSP. OPENED MCD AND R1 DOOR RAN PACKS TO VENT ACFT. ACFT NOW CLEAR OF DEICE FLUID HAZE.

Part: UPLOCK — FAILED (MLG) · airframe 44,141 hrs · 19,291 cycles

ON TAKEOFF WITH GEAR HANDLE SELECTED UP- HEARD LOUD NOISE FROM UNDER ACFT AND NOSE GEAR DOOR LIGHT ON BOTH MAIN INDICATOR AND OVERHEAD INDICATOR. DURING AFTER TAKEOFF CHECKLIST WITH GEAR HANDLE POSITION TO NEUTRAL- NOSE GEAR CAME DOWN AND LOCKED. PUT HANDLE BACK TO UP POSITION, GEAR CAME UP WITH DOOR LIGHT ON. DURING APPROACH GEAR EXTENDED NORMALLY WITH ALL DOOR LIGHTS OUT. INSPECTED NOSE GEAR WELL AREA AND FOUND UPLOCK ASSY AFT MOUNT BROKEN. R/R NOSE GEAR UPLOCK ASSEMBLY IAW M/M 32-31-21-4 UP TO STEP B/5 OPS TEST. PERFORMED FREE FALL EXTENSION FUNCTIONAL CHECK AND NORMAL RETRACTION AND EXTENSION FUNCTIONAL CHECK. LEAK AND OPS CHECK GOOD. REF AMM. 32-33-00 AND 32-31-00.

Part: ANGLE — CRACKED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

AFT LOWER CARGO, FRAME 63A, LOWER CLOSE OUT ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-72-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,113 hrs · 18,640 cycles

FUSELAGE INTERNAL STRUCTURE BELOW THE CARGO COMPARTMENT FLOOR HAS CORROSION ON A SUPPORT ANGLE AT FRAME 35 LBL 55. REMOVED CORROSION & FOUND TO OUT OF LIMITS IAW SRM 51-31-20 & SRM 53-10-00. LOCATED, DRILLED & TRIMMED IAW SRM 51-72-10. INSTALLED NEW ANGLE IAW SRM 51-72-10.

Part: SKIN — DELAMINATED (ZONE 400) · airframe 43,113 hrs · 18,640 cycles

NR 1 PYLON PANEL 474 BR INNER SKIN IS DELAMINATED. REPAIRED NR 1 PYLON PANEL 474 BR BY REMOVING DAMAGE; CLEANING; PREPARING AREA AND APPLYING FIBERGLASS WET LAY-UP REPAIRED IAW 54-50-00 AND 51-77-10. INSTALLED SEAL IAW DWG A54515353 CURED REPAIR IAW SRM 51-77-10 AND EA 6-5480-127937. APPLIED PORE FILLER IAW SRM 51-77-00; PARA 6-A 94 EA 6-5480-127937.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,113 hrs · 18,640 cycles

FUSELAGE INTERNAL STRUCTURE & CARGO COMPARTMENT FLOOR FLANGE IS CORRODED UNDER & AROUND THE NUTPLATES AND NUTS FROM FRAMES 38-38.1 RBL 55. REMOVED CORROSION & FOUND TO OUT OF LIMITS IAW SRM 51-31-20 & SRM 53-10- 00. LOCATED, DRILLED, & TRIMMED IAW SRM 51-72-10 & DWG 14A53778338. PART MARKED AND INSTALLED NEW ANGLE IAW SRM 51-72-10 & DWG 14A53778338.

Part: SUPPORT BRACKET — CHAFED (ZONE 400) · airframe 43,113 hrs · 18,640 cycles

NR 1 ENGINE OUTBD FAN COWL; FORWARD EDGE ALIGNMENT PIN SUPPORT BRACKET IS CHAFED AT THE BOTTOM SURFACE. REMOVED DAMAGE IAW EA 6-7110-127946. FOUND TO BE WITHIN LIMITS IAW EA 6-7110-127946; VIEW A-A. PRIMED IAW SRM 51-23-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,113 hrs · 18,640 cycles

BULK CARGO COMPARTMENT, FLOOR SUPPORT ANGLE BETWEEN FRAME 69 AND FRAME 70; AT STRINGER 42R THRU STRINGER 44R HAS CORROSION AROUND 2 FASTENER HOLES. ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 51-10-00. NEW ANGLE MATERIAL ID A2557217220600, PO NR 650584.2. LOCATED AND DRILLED HOLES IAW CAD DWG NR 17A25572172, REV "G". INSTALLED IAW A300-600 SRM 51-40-21.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,113 hrs · 18,640 cycles

FUSELAGE SKIN FWD EDGE OF THE CARGO DOOR CUTOUT, 12 INCHES FROM THE LOWER FWD CORNER IS DENTED. REMOVED FASTENERS IAW SRM 51-40-21. REMOVED DAMAGE IAW SRM 53-13-12. FABRICATED THE DOUBLER & FILLER IAW SRM 53-13-12. ALODINED THE DOUBLER, FILLER & SKIN CUTOUT IAW SRM 51-21-10. PRIMED DOUBLER, FILLER & SKIN COUOUT IAW SRM 51-23-10. INSTALLED THE DOUBLER & FILLER IAW SRM 53-13-12, FIG 203. TOP COATED FILLER & DOUBLER IAW SRM 51-21-10.

Part: PANEL — CRACKED (NR 1 NACELLE) · airframe 43,113 hrs · 18,640 cycles

NR 1 PYLON PANEL 413 BL IS CRACKED IN THE CORNER UNDER THE SEAL. REMOVED SEAL RETAINERS AND SEALS IAW SRM 51-40-21; PG 5. STOP DRILLED CRACKS IAW SRM 54-52-51; PG 225; STEP E. FABRICATED DOUBLER AND INSTALLED IAW SRM 54-52-51; PGS 229 / 230. REINSTALLED SEAL RETAINERS AND SEAL IAW SRM 51-40-21; PG 5

Part: BEAM — CORRODED (CARGO DOOR) · airframe 43,113 hrs · 18,640 cycles

THE BULK CARGO DOOR LOWER SUPPORT WEB IS CORRODED AROUND THE NUTPLATES AND SKIN BETWEEN FRAMES C-67 AND C-69. REMOVED AND INSTALLED NUTPLATES REF SRM 51-40-21. REMOVED CORROSION REF SRM SRM 51-74-10 AND CHECKED LIMITS REF SRM 53-17-18. FOUND TO BE OUT OF LIMITS REF SRM 53-10-00. STRAP AND FITTING REMOVED AND INSTALLED REF SRM 51-40-21. REMOVED CORRODED BEAM REF SRM 51-40- 21. RECEIVED AND INSTALLED NEW BEAM IAW REF SRM 51-40-21.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 43,113 hrs · 18,640 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE 341 AB CENTER RIB IS CRACKED. REMOVED FASTENERS IAW A310 ARM 51-40-21. STOP DRILED CRACK IAW SRM 55-12-19. FABRICATED REPAIR ANGLE IAW SRM 51-71-40 & SRM 51-71-40. INSTALLED REPAIR ANGLE IAW SRM 51-71-40.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,113 hrs · 18,640 cycles

CABIN FLOOR BOARD 282 KF IS CRACKED. REPAIRED PANEL 282 KF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK PIT FLOOR PANEL 161 AF IS PUNCTURED AND CORRODED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK PIT FLOOR PANEL 161 GF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK PIT FLOOR PANEL 161 HF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK CARGO COMPARTMENT FLOOR PANEL 162 DF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 152 BF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 BF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 132 QF IS BROKEN INTO MULTIPLE PIECES. REPAIRED FLOOR PANEL 132 QF WITH FABRICATION OF NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 152 FF HAS DELAMINATION AND EDGE DAMAGE. REPAIRED PANEL 152 FF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 131 YF IS BROKEN ALONG THE EDGE OF THE PANEL. REPAIRED PANEL 131 YF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 131 ZF IS CRUSHED AT THE CORNERS OF THE PDU CUTOUT. REPAIRED PANEL 131 ZF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,113 hrs · 18,640 cycles

CABIN FLOOR PANEL 242 LK IS BROKEN. REPAIRED PANEL 242 LK WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 131 QF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 131 QF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 152 EF HAS A BROKEN CORNER AND IS MISSING AN INSERT. REPAIRED PANEL 152 EF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK PIT FLOOR PANEL 161 BF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 132 ZF HAS MULTIPLE PUNCTURES ON THE BACK AND IS CRACKED AT THE CORNER OF THE PDU CUTOUT. REPAIRED PANEL 132 ZF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 131 RF IS BROKEN AT THE PDU CUTOUT. REPAIRED PANEL 131 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 152 AF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 AF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK PIT FLOOR PANEL 161 GF IS PUNCTURED AND CORRODED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: SILL — CORRODED (FUSELAGE) · airframe 43,113 hrs · 18,640 cycles

MAIN DECK, R-2 DOOR SILL AREA HAS A STRINGER ANGLE CORRODED AT FRAME 74, BS 3998 THRU 4005; STRINGER 26R. REMOVED CORROSION IN REF TO SRM 51-74-40. ORIGINAL MATERIAL THICKNESS 0.118 IAW DWG A539800712. MATERIAL REMOVED 0.026. MATERIAL REMANING 0.092 AND FOUND TO BE WITHIN LIMITS IAW DWG A537800712 AND SRM 53-10-00 FIG 104. ALODINED IN REF TO SRM 561-21-10. PRIMED & TOP COATED IAW SRM 51-23-10. REAPPLIED CIC IAW AMM 51-22-00-0; FIG 001.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 132 RF IS CRACKED AT THE PDU CUTOUT. REPAIRED PANEL 132 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,113 hrs · 18,640 cycles

CABIN FLOOR PANEL 241 LK. REPAIRED PNL 241LK WITH FABRICATION OF NEW PANEL. USING OLD PNL AS TEMPLATE IAW SRZ 25-005 REV H.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

AFT CARGO PIT SLANT PANEL 161 CW HAS SEVERAL PUNCTURES. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW DWG SRZ 25-005, REV "H" & DWG SRZ 25-011, REV "C".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,113 hrs · 18,640 cycles

BULK CARGO COMPARTMENT FLOOR PANEL 162 HF IS CRACKED AND CORRODED ON THE BACK OF THE PANEL. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,113 hrs · 18,640 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 132 YF IS CRUSHED ALONG THE EDGE AND HAS A BROKEN INSERT. REPAIRED PANEL 132 YF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,113 hrs · 18,640 cycles

THE MAIN DECK FLOORBEAMS ARE CORRODED AT FRAME C-14; RBL 36. REMOVED CORROSION IN REF TO SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15. REMOVED FLOORBEAM IAW SRM 51-72-10 PG 2. DRILLED NEW SUPPORT IAW SRM 51-72-10 PG 2. INSTALLED NEW FLOORBEAM SUPPORT IAW SRM 51-40-21& SRM 51-72-10 PG 2.

Part: CONTROL UNIT — SMOKE (COCKPIT) · airframe 43,067 hrs · 18,610 cycles

AT FL 330, ATS LEVER DROPPED OFF, NR 1 A/P DROPPED OFF ALONG WITH A PUFF OF SMOKE VISIBLE BE GLARESHIELD FLOOD LIGHTS. ATS RE-ENGAGED AS DID THE NR 1 A/P. NO FURTHER "PUFFS" OF SMOKE. NO FURTHER PROBLEMS. PERFORMED MTP AFS BITE AND FMC BITE, BOTH FAULTED FCU LAST FLIGHT. REMOVED FCU AND NOTED BURNT SMELL FROM AFT VENT HOLE OF FCU. INSPECTED FCU CONNECTOR AND C/P PINS. NO FAULTS NOTED. INSTALLED NEW FCU PER AMM 22-15-12-4. PERFORMED AFS/LAND TEST PER AMM 22-40-00-5. ALL OPS CK OK. ACFT OK TO CONTINUE. DOWNGRADED A/P NR 1 TO CK II PRECAUTIONARY AND A/P NR 2 REMAINS CAT II.

Part: PITOT LINE — OBSTRUCTED · airframe 42,851 hrs · 18,473 cycles

REJECTED TAKEOFF, NO AIRSPEED ON F/O'S PFD (60KTS). REMOVED LINE AT F/O'S PITOT PROBE AND PRESSURIZED WITH NITROGEN. THERE WAS A BLOCKAGE AT FIRST THEN IT CLEARED, WAS NOT ABLE TO DETERMINE WHAT THE BLOCKAGE WAS, BUT F/O'S PITOT PROBE IS NOW CLEAR. RECONNECTED LINE. SYSTEM OPS CHECKS NORMAL PER M/M 34-11-34-4. PERFORMED LEAK CHECK OF F/O'S PITOT SYSTEM, LEAK WAS GOOD PER M/M 34-10-10-501.

Part: ADC — FAILED (NR 2) · airframe 42,851 hrs · 18,473 cycles

ON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FROM ADC ARE NORMAL. THE ON ISSUE IS THE SEED. PER FLIGHT CREW THE SPEED STOP AND THERE WAS DIFFERENCE FROM THE CAPTAIN'S AND THE FO'S. DURING FLIGHT FROM OAK TO BUR, FLIGHT CREW DID MENTIONED THAT THEY SWITCHED OVER FROM NR 2 SGU TO NR 3 AND THE RESULTS WERE NO JOY. BAGGED FO'S PITOT PROBE AND BACK PRESSURED PITOT LINE, NO DEBRIS FOUND, RECONNECTED ALL LINES. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED FO'S PITOT LEAK CHECK WITH BARFIELD TESTER, LEAK CHECKS NORMAL. SYSTEM OPS CHECKS NORMAL PER MM 34-11-34-4.

Part: ADC — FAILED (NR 2) · airframe 42,851 hrs · 18,473 cycles

ON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FROM ADC ARE NORMAL. THE ON ISSUE IS THE SEED. PER FLIGHT CREW THE SPEED STOP AND THERE WAS DIFFERENCE FROM THE CAPTAIN'S AND THE F/O'S. DURING FLIGHT FROM OAK TO BUR, FLIGHT CREW DID MENTION THAT THEY SWITCHED OVER FROM NR 2 SGU TO NR 3 AND THE RESULTS WERE NO JOY. BAGGED F/O'S PITOT PROBE AND BACK PRESSURIZED PITOT LINE, NO DEBRIS FOUND, RECONNECTED ALL LINES. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED F/O'S PITOT LEAK CHECK WITH BARFIELD TESTER, LEAK CHECKS NORMAL. SYSTEM OPS CHECKS NORMAL PER M/M 34-11-34-4.

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY) · airframe 41,192 hrs · 17,482 cycles

ON TAKEOFF FROM IND, AT 50' FEET ROTATE MIN EQUIPMENT BAY SMOKE CAME ON. CHECKED THE SNIFFER FAN, DECLARED EMERGENCY AND CAME BACK AND LANDED. THE ECAM ALERT WENT AWAY ON TURN TO FINAL. NO ODOR WAS NOTED IN FWD EQUIPMENT BAY OR ANY OF THE LISTED COMPONENTS. CHECKED ALL AREAS FOR WATER. NONE FOUND. INSTALLED NEW MIN EQUIP BAY SMOKE DETECTOR 12WA PER MM 26-15-12-4 AND CHECKED GOOD PER MM 26-15-00-5. OK FOR SERVICE.

Part: FRAME — CRACKED (ZONE 100) · airframe 41,149 hrs · 17,462 cycles

DEVIATIONS DURING ACCOMPLISHMENT OF SB A310-57-2035 REV 8 AT INTERNAL ANGLE OF CENTER WING BOX. REPAIR PERFORMED BY OVERSIZING AFFECTED HOLES IAW EA 6-5710-103421 AND RAS/048070/031/2006 ISSUE "A".

Part: ATTACH FITTING — DAMAGED (ZONE 100) · airframe 41,148 hrs · 17,461 cycles

OLD MISDRILLED HOLE IN THE CLIP AT C68 LT, P42-P43, CLIP SHOWN IN SRM 553-17-13/FIG.9/SH.13/ITEM420. REPAIR PERFORMED BY REPLACEMENT OF AFFECTED STRUCTURE COMPONENT IAW SRM 51-72-10.

Part: FRAME — CORRODED (ZONE 300) · corrosion level 2 · airframe 41,149 hrs · 17,462 cycles

FUSELAGE TAIL SECTION, CORROSION AT C102, BETWEEN P13 LT AND P13 RT. REPAIR WAS PERFORMED BY TRIM THE FRAME OUTER FLANGE TO ALLOW FASTENER INSTALLATION.

Part: STRUT — CORRODED (ZONE 300) · airframe 41,148 hrs · 17,461 cycles

FOUND CORROSION ON CROSS STRUTS AT C87 RT AND LT. REPAIR PERFORMED BY REPLACEMENT WITH NEW PARTS IAW SRM 51-72-10.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 41,148 hrs · 17,461 cycles

OLD CORROSION REPAIRS ON TOP WING SKIN LT BETWEEN RIB 8 AND RIB 19, P12-15. OLD BLEND REPAIRS ARE WITHIN LIMITS GIVEN FROM AI EA 6-5720-103417 AND RAS/BAE/1003706/2006 ARE VALID FOR THIS SUBJECT.

Part: STRUCTURE — CORRODED (ZONE 500) · corrosion level 2 · airframe 41,149 hrs · 17,462 cycles

OUTER WING, CORROSION ON OVERWING REFUELING PORT LT. REPAIR WAS PERFORMED BY CORROSION REWORK IAW EA 6-5720-103412 AND RAS/BAE/1003838/2006 ISSUE "A".

Part: FLANGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 41,148 hrs · 17,461 cycles

CORROSION AT HOLES 34A AND 36A OF RT OUTBOARD HORIZONTAL FLANGE OF LOWER TEE SECTION. REPAIR CONSISTS OF OVERSIZING HOLES UP TO CORROSION REMOVAL AND INSTALLING REPAIR FASTENERS IAW EA 6-5710-103425 AND RAS/048047/009/2006 ISSUE "A".

Part: TRACK — DAMAGED (ZONE 100) · airframe 41,149 hrs · 17,462 cycles

MISDRILLED HOLE ON ROLLERTRACK AT C62 RT, Y-1470. REPAIR WAS PERFORMED BY REAM UP AND INSTALL FREEZE PLUGS IAW EA 6-5317-106354 REV A AND RAS/DATLS/0003496/2006 ISSUE "B".

Part: PRESSURE PANEL — DAMAGED (NLG WW) · airframe 41,149 hrs · 17,462 cycles

FASTENER CAN'T BE INSTALLED AT AFT NOSE LANDING GEAR PANEL, C17-18, P52-53 RT. REPAIR WAS PERFORMED BY FASTENER SUBSTITUTION IAW EA 6-5312-103408 REV A.

Part: FRAME — CRACKED (ZONE 100) · airframe 41,149 hrs · 17,462 cycles

DEVIATIONS DURING ACCOMPLISHMENT OF SB A310-57-2035 REV.8 AT INTERNAL ANGLE OF CENTER WING BOX. REPAIR PERFORMED BY OVERSIZING AFFECTED HOLES IAW EA 6-5710-103421 AND RAS/048070/031/2006 ISSUE "A".

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 17,462 cycles

CORROSION IN THE AIR CONDITIONING COMPARTMENT AT C42, P50-51 LT. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLING A REPAIR ANGLE AND A NEW PICK UP ANGLE IAW EA 6-5315-103434 AND RAS/048419/005/2006 ISSUE "A".

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 17,462 cycles

CORROSION IN THE AIR CONDITIONING COMP, C43-44, P47 RT. REPAIR WAS PERFORMED BY REWORK OF CORRODED AREA IAW EA 6-5315-103434 AND RAS/048419/005/2006 ISSUE "A".

Part: BEAM — CRACKED (ZONE 800) · airframe 41,148 hrs · 17,461 cycles

CRACKS IN 2 STAY, PROFILES AT C67A AND C68 RT BETWEEN BEAM 3-5, SHOWN IN SRM 52-34-00/FIG 2/PG 8) REPAIR PERFORMED BY REPLACEMENT OF AFFECTED STRUCTURE COMPONENT IAW SRM 51-72-10.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 17,462 cycles

FOUND CORROSION IN THE AIR CONDITIONING COMP, C42, P50-51 RT. REPAIR WAS PERFORMED BY CUT OUT AND INTALLING A REPAIR ANGLE AND A NEW PICK UP ANGLE IAW EA 6-5315-103434 AND RAS/048419/005/2006 ISSUE "A".

Part: SKIN — DELAMINATED (ZONE 500) · airframe 41,149 hrs · 17,462 cycles

CORROSION AND DELAMINATION ON T/E BOTTOM SURFACE LT WING. REPAIR WAS PERFORMED BY INSTALLING A NEW WEDGE SECTION AND A REPAIR PLATE IAW EA 6-5750-103433 AND RAS/BAE/1003821/2006 ISSUE "A".

Part: STRINGER — DAMAGED (ZONE 100) · airframe 41,149 hrs · 17,462 cycles

FWD KARMAN STRUCTURE C36-37 MISDRILLED HOLE AT STRINGER A535-43033-207. REPAIR WAS PERFORMED IAW EA 6-5314-103429 AND RAS/SA/111/2006 ISSUE "A".

Part: SLAT TRACK — WORN (ZONE 500) · airframe 41,149 hrs · 17,462 cycles

WEAR AT SLAT NR 3 LT, TRACK NR 9. REPAIR WAS PERFORMED IAW SRM 57-40-00 PB 101 AND APPROVED BY EA 6-5741-103381.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,149 hrs · 17,462 cycles

SKIN HAS DAMAGED AREA AROUND HOLE NR 12, C73-76, P26 RT, REPAIR WAS PERFORMED BY REAMING UP AND INSTALL A FREEZE PLUG IAW EA 6-5318-103403 REV A AND RAS/DAHAM/4021374/2006 ISSUE "C".

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORROSION AT STRINGER P56, C54.1-54.3. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201A AND NEW COUPLING INSTALLED.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,138 hrs · 17,458 cycles

FOUND CORROSION AT SERVICE BOX PANEL DOUBLER C12-12A LT. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5312-103410 AND RAS/AS/177/2006 ISSUE "A".

Part: SKIN — DAMAGED (ZONE 200) · airframe 41,143 hrs · 17,459 cycles

OVERSIZED HOLES FOUND DURING ACCOMPLISHMENT OF SB A310-53-2072 ON WING CENTER SECTION UPPER SURFACE STIFFENER 9 AND 10. REPAIR CONSISTS OF INSTALLING OF BOTH HOLES EN 6115-V5X IN TRANSITION FIT IAW EA 6-5315-103426 AND RAS 048117/009/2006 ISSUE "A".

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CROSSBEAM C62 RT CORRODED. REPAIR WAS PERFORMED BY REPLACEMENT OF CROSS BEAM IAW SRM 51-72-10.

Part: SKIN — CRACKED (ZONE 500) · airframe 41,138 hrs · 17,458 cycles

CRACKS AT 2 FASTENER HOLES AT AILERON HINGE RIB BOTTOM SKIN, LT WING. REPAIR WAS PERFORMED IAW EA 6-5720-103409 AND RAS/BAE/1003670/2006 ISSUE "A".

Part: ATTACH FITTING — DENTED (ZONE 500) · airframe 41,138 hrs · 17,458 cycles

NICK IN PYLON ATTACH FITTTING AND PYLON REINFORCEMENT PLATE. REPAIR WAS PERFORMED IAW EA 6-5720-103365 AND RAS/BAE/1003600/2006 ISSUE "A" (BLEND OUT).

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND DAMAGED HOLES ON LT WING TOP SKIN, REAR SPAR, RIB 4-5. REPAIR WAS PERFORMED BY REAMING UP HOLE 248 IAW EA 6-5720-103430 AND RAS/BAE/1003766/2006 ISSUE "A".

Part: FRAME — CORRODED (ZONE 300) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORROSION AT FRAME SECTION C102. PART REPLACED IAW SRM 51-72-10.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND TOP CAP BEAM C25 AD UPPER FLANGE A537-73651-210 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

SCRATCHES CLOSE TO STATIC PORT C27-29, P41 RT. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-103422 AND RAS/DATLS/0003445/2006 ISSUE "A".

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORROSION AT CROSS BEAM C63 LT. CROSS BEAM REPAIRED IAW SRM 53-10-15, PAGE 241/242.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

SCRATCHES ON SKIN AT C33-34, P54 RT TO P54 LT. REPAIR WAS PERFORMED BY INSTALLING AN EXTERNAL DOUBLER IAW EA 6-5314-103373 AND RAS/DABRE/7007106/2006 ISSUE "A".

Part: SPAR — CRACKED (CENTER WING BOX) · airframe 41,143 hrs · 17,459 cycles

CENTER WING BOX, CRACKS IN FLANGE SPAR NR 4 RT, C44.1. REPAIR WAS PERFORMED BY CUT OUT AND MANUFACTURE AND REPAIR ANGLE IAW EA 6-5710-103404 AND RAS/047737/009/2006 ISSUE "A".

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 41,138 hrs · 17,458 cycles

FOUND TWO DAMAGED HOLES (HOLE NR 4 RIB 17 AND HOLE NR 4 RIB 3-4) ON RT WING TOP SKIN AND CORROSION ON WING TOP SKIN. REPAIR WAS PERFORMED IAW EA 6-5720-106356 AND RAS/BAE/1003742/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,138 hrs · 17,458 cycles

FOUND CORROSION AT AFT NOSE LANDING GEAR PANEL C17-18, P52-53 RT. REPAIR WAS PERFORMED IAW EA 6-5312-103408 REV A AND RAS/AS/176/2006 ISSUE "A", SEE ALSO DRW R536-11104, CHANGED STRINGER, EXTERNAL DOUBLER INSTALLED AND DENT ACCEPTED.

Part: STRUCTURE — CORRODED (ZONE 300) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORRODED L-SECTION AT C95. REPAIR WAS PERFORMED BY FRAME CUT AND SPLICE IAW EA 6-5319-103401 AND RAS/DATLS/0003411/2006 ISSUE "A".

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 41,143 hrs · 17,459 cycles

CRACKED HOLE ON PYLON NR 2 AT RIB 8 UPPER SPAR. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201 AND APPROVED BY EA 6-5451-103400.

Part: ANGLE — CRACKED (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

FUSELAGE CENTER SECTION, CRACKED HOLE AT PICK UP ANGLE, C39-40 RT. REPAIR WAS PERFORMED BY OVERSIZING AND BUSHING INSTALLATION IAW EA 6-5315-103413 AND RAS/AS/0212/2006 ISSUE "A".

Part: ATTACH FITTING — DAMAGED (ZONE 100) · airframe 41,138 hrs · 17,458 cycles

LT NOSE GEAR DOOR ATTACHMENT FITTING DAMAGED. REPLACEMENT OF ATTACHMENT FITTING IAW AMM 32-31-16.

Part: PLATE — DAMAGED (ZONE 600) · airframe 41,143 hrs · 17,459 cycles

NICK IN PYLON REINFORCEMENT PLATE RT. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5720-103365.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORROSION AT CROSSBEAM C67 RT. PART REPLACED IAW SRM 51-72-10.

Part: ANGLE — CORRODED (ZONE 300) · airframe 41,138 hrs · 17,458 cycles

CORROSION BETWEEN C91 AND C92 BILGE AREA AT OUTER FLANGE C91, SOME ANGLES C92 AND AT DOUBLER P23 C92. REPAIR WAS PERFORMED BY REMOVING CORROSION IAW SRM51-74-10 AND REPLACEMENT OF CORRODED STRUCTURE PARTS IAW SRM 51-72-10, SRM 53-19-18/FIG 9 AND SRM 5319-13/FIG 11/12.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORRODED CLIP AT C35, P43-44 RH. CLIP REPLACED IAW SRM 51-72-10.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

DOUBLE HOLE IN SKIN AT C73-74, P28 LT. REPAIR WAS PERFORMED BY REAM UP THE HOLE IAW EA 6-5318-103397 AND RAS/DATLS/0003407/2006 ISSUE "A".

Part: STRINGER — DAMAGED (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

DEFORMATION OF STRINGER AT C65, P38 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORROSION ON COUPLING BETWEEN C54.2-54.3, P51 LT AND ON STRINGER P51 LT, C54.2. REPAIR WAS PERFORMED IAW SRM 53-10-14 AND SRM 51-72-10, STRINGER REPAIR AND COUPLING REPLACEMENT.

Part: FITTING — MAINT ERROR (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

OLD MISDRILLED HOLE AT FITTING C74, P26 RT. PART REPLACED IAW SRM 51-72-10.

Part: BRACKET — CRACKED (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

FOUND BRACKET A262-70471-200 BETWEEN CROSS BEAM C26/32 AND C33 CRACKED. BRACKET A262-70471-202 BETWEEN CROSS BEAM C33 AND 34 CRACKED. NEW PARTS INSTALLED IAW SRM 51-72-10.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 41,138 hrs · 17,458 cycles

FOUND CORROSION ON LT WING TOP SKIN. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5720-106356 AND RAS/BAE/1003742/2006 ISSUE "A".

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,143 hrs · 17,459 cycles

FOUND CORRODED SPLICE AT C19 P48 LT. PART REPLACED IAW SRM 51-72-10.

Part: FLOORBEAM — MAINT ERROR (ZONE 100) · airframe 41,143 hrs · 17,459 cycles

MISDRILLED HOLE IN THE FLOOR STRUCTURE OF FWD CARGO COMPARTMENT C22 RT. REPAIR WAS PERFORMED IAW EA 6-5313-103406 AND RAS/DABRE/7007121/2006 ISSUE "A". REPAIR ANGLE INSTALLED.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,138 hrs · 17,458 cycles

FOUND CORROSION AT L-PROFILE, C73-76, P26 RT. REPAIR WAS PERFORMED BY REMOVING CORROSION IAW EA 6-5318-103403 REV A AND RAS/DAHAM/4021374/2006 ISSUE "C".

Part: SKIN — CHAFED (ZONE 600) · airframe 41,138 hrs · 17,458 cycles

CHAFING MARKS TO LEADING EDGE 'D' NOSE SKIN, BOTH WINGS. LT WING BETWEEN TRACK 5 AND TRACK 6, LT WING BETWEEN TRACK 9 AND TRACK 10, RT WING BETWEEN TRACK 5 AND TRACK 6 AND RT WING AREA OF TRACK 1. REPAIR WAS PERFORMED BY BLENDING AND REPLACMENT IAW EA 6-5741-103419 AND RAS/BAE/1003686/2006 ISSUE "A".

Part: SKIN — CHAFED (ZONE 600) · airframe 41,138 hrs · 17,458 cycles

CHAFING MARKS TO LEADING EDGE 'D' NOSE SKIN, BOTH WINGS. LT WING BETWEEN TRACK 5 AND TRACK 6, LT WING BETWEEN TRACK 9 AND TRACK 10, RT WING BETWEEN TRACK 5 AND TRACK 6 AND RT WING AREA OF TRACK 1. REPAIR WAS PERFORMED IAW EA 6-5741-103419 AND RAS/BAE/1003686/2006 ISSUE "A".

Part: FITTING — MISREPAIRED (ZONE 500) · airframe 41,128 hrs · 17,455 cycles

OLD REPAIR ON CENTER WING FITTING C47, DEVIATION OF HOLE 1 AND 41 WITH SB 57-2047. VERIFICATION OF REPAIR, PERFORMED IAW RAS 013464/014/2001 ISSUE "A" AND SIA-EN: 10EN-57-7681.

Part: FITTING — DAMAGED (ZONE 300) · airframe 41,128 hrs · 17,455 cycles

OLD REPAIR ON LT ELEVATOR, AT INNER FITTING NR 2, A LUG IS BROKEN OFF TO INSTALL A SAFETY COTTER PIN. VISUAL VERIFICATION OF REPAIR, ACCOMPLISHED IAW RAS/CASA/2363/2002 ISSUE "A".

Part: SKIN — DELAMINATED (ZONE 500) · airframe 41,128 hrs · 17,455 cycles

DELAMINATION ON OLD DOUBLER REPAIR, LT INBOARD FLAP, AFT OF TRACK NR 2. REPAIR PERFORMED BY REMOVING THE EXISTING REPAIR AN INSTALL SRM REPAIR PER 57-53-12, FIG 209. APPROVED BY EA 6-5752-103366 AND RAS/DABRE/7007096/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 41,128 hrs · 17,455 cycles

OLD REPAIR ON LT WING ON TOP SKIN, REAR SPAR, BETWEEN RIB 4-5. VISUAL INSPECTION FOR FURTHER CORROSION AND CORRECT TAPERLOCK INSTALLATION IAW AMM570000/601/PARA 2, SRM514021/001/PARA 9 AND RAS/BAE/0439/98 ISSUE "B". (FURTHER DR422).

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 41,133 hrs · 17,456 cycles

FOUND CORROSION ON RT WING TOP SKIN AT TRAILING EDGE AREA OUTER SHROUD BOX. REPAIR PERFORMED IAW EA 6-5720-103382.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 41,133 hrs · 17,456 cycles

OLD DELAMINATION REPAIR ON INBOARD FLAP RT UPPER SURFACE AT TRAILING EDGE. REPAIR PERFORMED BY REPLACING THE EXISTING REPAIR IAW SRM 57-53-12/FIG 209 APPROVED BY EA 6-5752-103367 AND RAS/DABRE/7007093/2006 ISSUE "A".

Part: SLAT TRACK — CORRODED (ZONE 600) · corrosion level 2 · airframe 41,133 hrs · 17,456 cycles

FOUND CORROSION ON SLAT TRACK NR 7 INBOARD AT INNER LOWER SKIN. REPAIR PERFORMED IAW EA 6-5720-103412.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 41,124 hrs · 17,452 cycles

OLD CROSS BEAM REPAIR WHICH WAS NOT CONFORM TO SRM. THE SRM REPAIR IN SOURCE DR330 ISN'T APPLICABLE. ANOTHER CROSSBEAM REPAIR WAS NECESSARY. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15, FIG.207.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 41,124 hrs · 17,452 cycles

OLD DAMAGED STRINGER P37 LT BETWEEN C55/58 AND C59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14, FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,452 cycles

FOUND HEAVY CORROSION ON STRINGER P30 RT BETWEEN C33 AND C34. REPAIR IS PERFORMED IAW RAS/DABRE/7007241/2006 ISSUE:A (EA 6-5314-103372).

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 41,124 hrs · 17,452 cycles

OLD CROSSBEAM REPAIR AT C62 WHICH IS NOT CONFORM TO THE SRM. REPAIR PERFORMED IAW SRM 53-10-15, FIG 207, PERFORMED WITH FOLLOW DR511.

Part: SKIN — DAMAGED (ZONE 400) · airframe 41,124 hrs · 17,452 cycles

PYLON SUPPORT BRACKET HOLES ON LT/RT WING BOTTOM SKIN DAMAGED. REPAIR PERFORMED IAW EA 6-5720-103398.

Part: FITTING — LOOSE (ZONE 400) · airframe 41,124 hrs · 17,452 cycles

HYD FITTING GREEN PRESSURE PIPE AND BLUE SUCTION PIPE LOOSE IN FEED THROUGH ON LT WING. REPAIR PERFORMED IAW AI-INSTRUCTION: R572-49184 ISSUE: C (EA 6-5720-103398).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,452 cycles

FOUND HEAVY CORROSION ON STRINGER P30 RT BETWEEN C33 AND C34. REPAIR IS PERFORMED IAW RAS/DABRE/7007241/2006 ISSUE:A (EA 6-5314-103372).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,452 cycles

FOUND HEAVY CORROSION ON STRINGER WITH COUPLING AT C54.3, P49. REPAIR IS PERFORMED IAW SRM 53-10-14, FIG 201.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,452 cycles

FOUND CORROSION ON TOP CAP BEAM, UPPER FLANGE, C25 AD. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 207 AND SRM 51-72-10.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 41,124 hrs · 17,452 cycles

AT LOWER SKIN ON SPOILER 2 LT TRAILING EDGE WAS AN AREA DELAMINATED. REPAIR PERFORMED IAW EA 6-5770-103369.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,452 cycles

FOUND HEAVY CORROSION ON P44 RT BETWEEN C38.2-C39. REPAIR PERFORMED IAW SRM 53-10-14, FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,451 cycles

FOUND CORROSION OLD STRINGER REPAIR AT C42/43, P50 RT WASN'T ALLOWED IN AFFECTED AREA (RECHECK WITH SRM 53-10-14, FIG 201A). RENEW OF OLD REPAIR IAW SRM 53-10-14, FIG 201A. PERFORMED IAW RAS 048525/009/2006 ISSUE: A. (EA 6-5315-106344).

Part: SKIN — UNKNOWN (ZONE 200) · airframe 41,124 hrs · 17,451 cycles

OLD DOUBLER REPAIR ON SKIN BETWEEN C73A/C74, P28/29 RT VERIFICATION OF REPAIR, PERFORMED IAW RAS/DAHAM/4018650/2004 ISSUE: A. FOR NEW REQUIREMENTS SEE DR394 (EA6-5318-103411).

Part: PANEL — UNKNOWN (ZONE 100) · airframe 41,124 hrs · 17,451 cycles

OLD CORROSION REPAIR ON FRONT PANEL OF NOSE LANDING GEAR BAY. REPAIR VERIFICATION, PERFORMED IAW RAS/AS/073/02 ISSUE: A, EA FOR TRACKING: 6-5312-103346.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,124 hrs · 17,451 cycles

FOUND CORROSION, OLD STRINGER REPAIR AT C42/43, P50 RT. VERIFICATION SHOWS THAT REPAIR IS NOT CONFORM TO SRM 53-10-14, FIG 201A, SEC.A-A.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,119 hrs · 17,447 cycles

OLD CORROSION REPAIR IN FUSELAGE CENTER SECTION AT C39 AND CORROSION AT PRESSURE BULKHEAD. REPAIR WAS VERIFIED AND PERFORMED IAW RAS: 047609/013/2006 ISSUE:A.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,119 hrs · 17,447 cycles

FOUND CORROSION AT MANHOLE FITTING ( C38-C38.1) AND EXTERNAL SKIN AREA FWD OF C39. REPAIR WAS PERFORMED IAW TD/K7/S1/07107 ISS.A (EA 6-5314-106384A), APPROVED BY RAS/DABRE/7007107/2006 ISS.:A.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,119 hrs · 17,447 cycles

FOUND CORROSION SPOTS AFTER REMOVAL OF OLD EXTERNAL DOUBLER AT C18, P16/18 LT. REPAIR WAS PERFORMED IAW RAS/AS/165/2006 ISS.A ( EA 6-5312-103399) DR 508 IS ALSO COVERED BY MENTIONED RAS.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,119 hrs · 17,447 cycles

FOUND CORROSION SPOTS ON FUSELAGE SKIN PANEL AT BUTT-STRAP C18 BETWEEN P26-27 LT. REPAIR WAS PERFORMED IAW TD942.047408/017/2006A (EA 6-5312-103399) AND APPROVED BY RAS/AS/165/2006 ISSUE:A. SEE ALSO DR 186 WHICH IS PERFORMED WITH MENTIONED RAS.